发明名称 AIRCRAFT FUSELAGE DURABILITY TEST BENCH
摘要 FIELD: aircraft engineering.SUBSTANCE: this test bench comprises compressed air cyclic load system composed of compressed air source, compressed air main feed line with high-flow rate control valve, bypass line, line to discharge air from fuselage with release valve, means for protection of fuselage from compressed air overpressure and noise killer. Besides, it includes ACS means incorporating fuselage pressure controller and pressure first transducer. Additionally, it comprises "downstream" pressure controller at first bypass line, second bypass line parallel with inlet control valve incorporating manual and solenoid valves, inlet control valve opening correction unit, timer, command-apparatus, pressure level comparator and switch to control operation of control valve and the entire system of fuselage overpressure control.EFFECT: higher accuracy of fuselage overpressure control, expanded applications of test bench.2 dwg
申请公布号 RU2548054(C2) 申请公布日期 2015.04.10
申请号 RU20130136124 申请日期 2013.08.01
申请人 FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "TSENTRAL'NYJ AEHROGIDRODINAMICHESKIJ INSTITUT IMENI PROFESSORA N.E. ZHUKOVSKOGO" (FGUP "TSAGI") 发明人 KUTSENKO SERGEJ ALEKSANDROVICH;STERLIN ANDREJ JAKOVLEVICH;SINITSIN ANATOLIJ SEMENOVICH
分类号 G01M5/00 主分类号 G01M5/00
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